The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 20, 2017

Filed:

Jun. 25, 2015
Applicant:

Airbus Helicopters, Marignane, FR;

Inventor:

Marc Salesse-Lavergne, Allauch, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 13/18 (2006.01); G05D 1/08 (2006.01); B64C 27/04 (2006.01);
U.S. Cl.
CPC ...
B64C 13/18 (2013.01); B64C 27/04 (2013.01); G05D 1/0858 (2013.01);
Abstract

A flight control system for a rotary wing aircraft, the aircraft following a track T, relative to the ground with a ground course angle TK, a forward speed Va, a flight path angle P, and a heading Ψ, the aircraft having one or more rotary wings provided with blades of collective pitch and of cyclic pitch that are variable about respective pitch axes and that are capable of performing movements in rotation and in translation. The flight control system has two control members each provided respectively with at least one movement axis A, B, C, D, and an autopilot for generating control signals. An action on one of the control members relative to one of the movement axes A, B, C, D gives rise independently to a modification to the forward speed Va, to the ground course angle TK, or indeed to the flight path angle P by means of the autopilot.


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